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   <h4 class="subsectionHead"><span class="titlemark">2.7   </span> <a 
 id="x12-380002.7"></a>Axisymmetric Elements</h4>
<!--l. 1008--><p class="noindent" >Implementation relies on elements located exclusively in <span 
class="cmmi-10">x,y </span>plane. The coordinate <span 
class="cmmi-10">x </span>corresponds to radius, <span 
class="cmmi-10">y </span>is the
axis of rotation. Approximation of displacement functions <span 
class="cmmi-10">u,v </span>is carried out on a particular finite element. Nonzero
strains read <div class="eqnarray">
   <center class="math-display" >
<img 
src="elementlibmanual6x.png" alt="  &#x03B5;x = &#x03B5;r =  &part;u-                                     (1)
             &part;x
  &#x03B5;y = &#x03B5;z =  &part;v-                                     (2)
             &part;y
      &#x03B5;&#x03B8;  =  u-                                      (3)
             r
&gamma;xy = &gamma;rz =  &part;u-+ &part;v-                                (4)
             &part;y   &part;x
" class="math-display" ></center>
</div>Stress components can be computed from elasticity matrix. Note that this matrix corresponds to a submatrix of the
full 3D elasticity matrix. <div class="eqnarray">
   <center class="math-display" >
<img 
src="elementlibmanual7x.png" alt="(     )                 &lfloor;                              &rfloor;  (      )
||{  &sigma;x ||}                 | 1 &minus; &nu;   &nu;     &nu;        0     |  ||{   &#x03B5;x  ||}
   &sigma;y    = -----E-------|&lceil;   &nu;    1&minus; &nu;   &nu;        0     |&rceil; =    &#x03B5;y               (5)
||(  &sigma;&#x03B8; ||)    (1+ &nu;)(1 &minus; 2&nu;)    &nu;     &nu;    1&minus; &nu;      0        ||(   &#x03B5;&#x03B8;  ||)
   &sigma;xy                      0     0     0    (1&minus; 2&nu;)&#x2215;2       &gamma;xy
" class="math-display" ></center>
</div>In OOFEM, the strain vector is arranged as <span 
class="cmsy-10">{</span><span 
class="cmmi-10">&#x03B5;</span><sub><span 
class="cmmi-7">x</span></sub><span 
class="cmmi-10">,&#x03B5;</span><sub><span 
class="cmmi-7">y</span></sub><span 
class="cmmi-10">,&#x03B5;</span><sub><span 
class="cmmi-7">&#x03B8;</span></sub><span 
class="cmmi-10">,</span>0<span 
class="cmmi-10">,</span>0<span 
class="cmmi-10">,&gamma;</span><sub><span 
class="cmmi-7">xy</span></sub><span 
class="cmsy-10">}</span><sup><span 
class="cmmi-7">T</span></sup> and the stress vector <span 
class="cmsy-10">{</span><span 
class="cmmi-10">&sigma;</span><sub><span 
class="cmmi-7">x</span></sub><span 
class="cmmi-10">,&sigma;</span><sub><span 
class="cmmi-7">y</span></sub><span 
class="cmmi-10">,&sigma;</span><sub><span 
class="cmmi-7">&#x03B8;</span></sub><span 
class="cmmi-10">,</span>0<span 
class="cmmi-10">,</span>0<span 
class="cmmi-10">,&tau;</span><sub><span 
class="cmmi-7">xy</span></sub><span 
class="cmsy-10">}</span><sup><span 
class="cmmi-7">T</span></sup>.
Implementation assumes a segment of 1 rad.
<!--l. 1023--><p class="noindent" >
   <h5 class="subsubsectionHead"><span class="titlemark">2.7.1   </span> <a 
 id="x12-390002.7.1"></a>Axisymm3d element</h5>
<!--l. 1024--><p class="noindent" >Implementation of triangular three-node finite element for axisymmetric continuum. Each node has 2 degrees of
freedom. Node numbering and edge position is the same as in Fig.&#x00A0;<a 
href="elementlibmanualsu4.html#x9-170017">7<!--tex4ht:ref: TrPlanestressfig --></a>. The element features are summarized in
Table&#x00A0;<a 
href="#x12-3900130">30<!--tex4ht:ref: axisymm3dsummary --></a>.
                                                                                           
                                                                                           
<div class="center" 
>
<!--l. 1029--><p class="noindent" >
<div class="table">
<!--l. 1029--><p class="noindent" ><a 
 id="x12-3900130"></a><hr class="float"><div class="float" 
> <!--tex4ht:inline--><div class="tabular"> <table id="TBL-31" class="tabular" 
cellspacing="0" cellpadding="0" rules="groups" 
><colgroup id="TBL-31-1g"><col 
id="TBL-31-1"></colgroup><colgroup id="TBL-31-2g"><col 
id="TBL-31-2"></colgroup><tr 
class="hline"><td><hr></td><td><hr></td></tr><tr  
 style="vertical-align:baseline;" id="TBL-31-1-"><td  style="white-space:nowrap; text-align:left;" id="TBL-31-1-1"  
class="td11"><span 
class="cmbx-10">Keyword         </span></td><td  style="white-space:wrap; text-align:left;" id="TBL-31-1-2"  
class="td11"><!--l. 1029--><p class="noindent" ><span 
class="cmbx-10">Axisymm3d</span>                                                   </td>
</tr><tr  
 style="vertical-align:baseline;" id="TBL-31-2-"><td  style="white-space:nowrap; text-align:left;" id="TBL-31-2-1"  
class="td11">Description          </td><td  style="white-space:wrap; text-align:left;" id="TBL-31-2-2"  
class="td11"><!--l. 1029--><p class="noindent" >Triangular axisymmetric linear element                         </td>
</tr><tr  
 style="vertical-align:baseline;" id="TBL-31-3-"><td  style="white-space:nowrap; text-align:left;" id="TBL-31-3-1"  
class="td11">Specific parameters</td><td  style="white-space:wrap; text-align:left;" id="TBL-31-3-2"  
class="td11"><!--l. 1029--><p class="noindent" >[<span 
class="cmtt-10">NIP</span>&#x00A0;#<span 
class="cmr-5">(in)</span>] [<span 
class="cmtt-10">NIPfish</span>&#x00A0;#<span 
class="cmr-5">(in)</span>]                                          </td>
</tr><tr 
class="hline"><td><hr></td><td><hr></td></tr><tr  
 style="vertical-align:baseline;" id="TBL-31-4-"><td  style="white-space:nowrap; text-align:left;" id="TBL-31-4-1"  
class="td11">Parameters           </td><td  style="white-space:wrap; text-align:left;" id="TBL-31-4-2"  
class="td11"><!--l. 1030--><p class="noindent" ><span 
class="cmtt-10">NIP</span>: allows to set the number of integration points (possible
completions are 1 (default), 4 and 7 point integration rule).</td>
</tr><tr  
 style="vertical-align:baseline;" id="TBL-31-5-"><td  style="white-space:nowrap; text-align:left;" id="TBL-31-5-1"  
class="td11">Unknowns            </td><td  style="white-space:wrap; text-align:left;" id="TBL-31-5-2"  
class="td11"><!--l. 1031--><p class="noindent" >Two dofs (u-displacement, v-displacement) are required in
each node.                                                               </td>
</tr><tr  
 style="vertical-align:baseline;" id="TBL-31-6-"><td  style="white-space:nowrap; text-align:left;" id="TBL-31-6-1"  
class="td11">Approximation      </td><td  style="white-space:wrap; text-align:left;" id="TBL-31-6-2"  
class="td11"><!--l. 1032--><p class="noindent" >Linear approximation of displacement and geometry.        </td>
</tr><tr  
 style="vertical-align:baseline;" id="TBL-31-7-"><td  style="white-space:nowrap; text-align:left;" id="TBL-31-7-1"  
class="td11">Integration           </td><td  style="white-space:wrap; text-align:left;" id="TBL-31-7-2"  
class="td11"><!--l. 1033--><p class="noindent" >The integration can be altered using <span 
class="cmtt-10">NIP </span>paramter (default
is 1 point integration).                                               </td>
</tr><tr  
 style="vertical-align:baseline;" id="TBL-31-8-"><td  style="white-space:nowrap; text-align:left;" id="TBL-31-8-1"  
class="td11">Features              </td><td  style="white-space:wrap; text-align:left;" id="TBL-31-8-2"  
class="td11"><!--l. 1034--><p class="noindent" >-                                                                            </td></tr><tr  
 style="vertical-align:baseline;" id="TBL-31-9-"><td  style="white-space:nowrap; text-align:left;" id="TBL-31-9-1"  
class="td11">CS properties </td> <td  style="white-space:wrap; text-align:left;" id="TBL-31-9-2"  
class="td11"><!--l. 1035--><p class="noindent" >-</td>
</tr><tr  
 style="vertical-align:baseline;" id="TBL-31-10-"><td  style="white-space:nowrap; text-align:left;" id="TBL-31-10-1"  
class="td11">Loads                  </td><td  style="white-space:wrap; text-align:left;" id="TBL-31-10-2"  
class="td11"><!--l. 1036--><p class="noindent" >Boundary and body loads are supported.                       </td>
</tr><tr  
 style="vertical-align:baseline;" id="TBL-31-11-"><td  style="white-space:nowrap; text-align:left;" id="TBL-31-11-1"  
class="td11">Nlgeo                  </td><td  style="white-space:wrap; text-align:left;" id="TBL-31-11-2"  
class="td11"><!--l. 1037--><p class="noindent" >0.                                                                          </td>
</tr><tr  
 style="vertical-align:baseline;" id="TBL-31-12-"><td  style="white-space:nowrap; text-align:left;" id="TBL-31-12-1"  
class="td11">Status                 </td><td  style="white-space:wrap; text-align:left;" id="TBL-31-12-2"  
class="td11"><!--l. 1038--><p class="noindent" >-                                                                            </td></tr><tr  
 style="vertical-align:baseline;" id="TBL-31-13-"><td  style="white-space:nowrap; text-align:left;" id="TBL-31-13-1"  
class="td11"> </td>
</tr><tr 
class="hline"><td><hr></td><td><hr></td></tr><tr  
 style="vertical-align:baseline;" id="TBL-31-14-"><td  style="white-space:nowrap; text-align:left;" id="TBL-31-14-1"  
class="td11">                </td></tr></table></div>
<br /> <div class="caption" 
><span class="id">Table&#x00A0;30: </span><span  
class="content">Axisymm3d element summary</span></div><!--tex4ht:label?: x12-3900130 -->
</div><hr class="endfloat" />
</div>
</div>
<!--l. 1041--><p class="noindent" >
   <h5 class="subsubsectionHead"><span class="titlemark">2.7.2   </span> <a 
 id="x12-400002.7.2"></a>Q4axisymm element</h5>
<!--l. 1042--><p class="noindent" >Implementation of quadratic isoparametric eight-node quadrilateral - finite element for axisymmetric 3d continuum.
Each node has 2 degrees of freedom. The element features are summarized in Table&#x00A0;<a 
href="#x12-4000131">31<!--tex4ht:ref: q4axisymmsummary --></a>.
<div class="center" 
>
<!--l. 1046--><p class="noindent" >
<div class="table">
<!--l. 1046--><p class="noindent" ><a 
 id="x12-4000131"></a><hr class="float"><div class="float" 
> <!--tex4ht:inline--><div class="tabular"> <table id="TBL-32" class="tabular" 
cellspacing="0" cellpadding="0" rules="groups" 
><colgroup id="TBL-32-1g"><col 
id="TBL-32-1"></colgroup><colgroup id="TBL-32-2g"><col 
id="TBL-32-2"></colgroup><tr 
class="hline"><td><hr></td><td><hr></td></tr><tr  
 style="vertical-align:baseline;" id="TBL-32-1-"><td  style="white-space:nowrap; text-align:left;" id="TBL-32-1-1"  
class="td11"><span 
class="cmbx-10">Keyword         </span></td><td  style="white-space:wrap; text-align:left;" id="TBL-32-1-2"  
class="td11"><!--l. 1046--><p class="noindent" ><span 
class="cmbx-10">Q4axisymm</span>                                                   </td>
</tr><tr  
 style="vertical-align:baseline;" id="TBL-32-2-"><td  style="white-space:nowrap; text-align:left;" id="TBL-32-2-1"  
class="td11">Description          </td><td  style="white-space:wrap; text-align:left;" id="TBL-32-2-2"  
class="td11"><!--l. 1046--><p class="noindent" >Quadratic   isoparametric   eight-node   quadrilateral   for
axisymmetric analysis                                                </td>
</tr><tr  
 style="vertical-align:baseline;" id="TBL-32-3-"><td  style="white-space:nowrap; text-align:left;" id="TBL-32-3-1"  
class="td11">Specific parameters</td><td  style="white-space:wrap; text-align:left;" id="TBL-32-3-2"  
class="td11"><!--l. 1046--><p class="noindent" >[<span 
class="cmtt-10">NIP</span>&#x00A0;#<span 
class="cmr-5">(in)</span>] [<span 
class="cmtt-10">NIPfish</span>&#x00A0;#<span 
class="cmr-5">(in)</span>]                                          </td>
</tr><tr 
class="hline"><td><hr></td><td><hr></td></tr><tr  
 style="vertical-align:baseline;" id="TBL-32-4-"><td  style="white-space:nowrap; text-align:left;" id="TBL-32-4-1"  
class="td11">Parameters           </td><td  style="white-space:wrap; text-align:left;" id="TBL-32-4-2"  
class="td11"><!--l. 1047--><p class="noindent" ><span 
class="cmtt-10">NIP</span>:  allows  to  set  the  number  of  integration  points  for
integration  of  terms  corresponding  to  <span 
class="cmmi-10">&#x03B5;</span><sub><span 
class="cmmi-7">x</span></sub>  and  <span 
class="cmmi-10">&#x03B5;</span><sub><span 
class="cmmi-7">y</span></sub>  strains
(possible completions are 1, 4 (default), 9, and 16).          </td>
</tr><tr  
 style="vertical-align:baseline;" id="TBL-32-5-"><td  style="white-space:nowrap; text-align:left;" id="TBL-32-5-1"  
class="td11">                </td><td  style="white-space:wrap; text-align:left;" id="TBL-32-5-2"  
class="td11"><!--l. 1049--><p class="noindent" ><span 
class="cmtt-10">NIPfish</span>: allows to set the number of integration points
for integration of remain terms (corresponding to <span 
class="cmmi-10">&#x03B5;</span><sub><span 
class="cmmi-7">&#x03B8;</span></sub> and
<span 
class="cmmi-10">&gamma;</span><sub><span 
class="cmmi-7">rz</span></sub>) (Supported values include 1 (default), 4, 9, and 16
integration point formula).                                          </td>
</tr><tr  
 style="vertical-align:baseline;" id="TBL-32-6-"><td  style="white-space:nowrap; text-align:left;" id="TBL-32-6-1"  
class="td11">Unknowns            </td><td  style="white-space:wrap; text-align:left;" id="TBL-32-6-2"  
class="td11"><!--l. 1050--><p class="noindent" >Two dofs (u-displacement, v-displacement) are required in
each node.                                                               </td>
</tr><tr  
 style="vertical-align:baseline;" id="TBL-32-7-"><td  style="white-space:nowrap; text-align:left;" id="TBL-32-7-1"  
class="td11">Approximation      </td><td  style="white-space:wrap; text-align:left;" id="TBL-32-7-2"  
class="td11"><!--l. 1051--><p class="noindent" >Quadratic approximation of displacement and geometry.   </td>
</tr><tr  
 style="vertical-align:baseline;" id="TBL-32-8-"><td  style="white-space:nowrap; text-align:left;" id="TBL-32-8-1"  
class="td11">Integration           </td><td  style="white-space:wrap; text-align:left;" id="TBL-32-8-2"  
class="td11"><!--l. 1052--><p class="noindent" >The integration of terms corresponding to <span 
class="cmmi-10">&#x03B5;</span><sub><span 
class="cmmi-7">x</span></sub> and <span 
class="cmmi-10">&#x03B5;</span><sub><span 
class="cmmi-7">y</span></sub> strains
can  be  altered  using  <span 
class="cmtt-10">NIP </span>parameter  (default  is  4  point
formula). The remaining terms (creesponding to <span 
class="cmmi-10">&#x03B5;</span><sub><span 
class="cmmi-7">&#x03B8;</span></sub> and <span 
class="cmmi-10">&gamma;</span><sub><span 
class="cmmi-7">rz</span></sub>)
are integrated by default using 1 point formula (see <span 
class="cmtt-10">NIPfish</span>
parameter).                                                             </td>
</tr><tr  
 style="vertical-align:baseline;" id="TBL-32-9-"><td  style="white-space:nowrap; text-align:left;" id="TBL-32-9-1"  
class="td11">Features              </td><td  style="white-space:wrap; text-align:left;" id="TBL-32-9-2"  
class="td11"><!--l. 1053--><p class="noindent" >-                                                                            </td></tr><tr  
 style="vertical-align:baseline;" id="TBL-32-10-"><td  style="white-space:nowrap; text-align:left;" id="TBL-32-10-1"  
class="td11">CS properties </td> <td  style="white-space:wrap; text-align:left;" id="TBL-32-10-2"  
class="td11"><!--l. 1054--><p class="noindent" >-</td>
</tr><tr  
 style="vertical-align:baseline;" id="TBL-32-11-"><td  style="white-space:nowrap; text-align:left;" id="TBL-32-11-1"  
class="td11">Loads                  </td><td  style="white-space:wrap; text-align:left;" id="TBL-32-11-2"  
class="td11"><!--l. 1055--><p class="noindent" >No boundary and body loads are supported.                   </td>
</tr><tr  
 style="vertical-align:baseline;" id="TBL-32-12-"><td  style="white-space:nowrap; text-align:left;" id="TBL-32-12-1"  
class="td11">Nlgeo                  </td><td  style="white-space:wrap; text-align:left;" id="TBL-32-12-2"  
class="td11"><!--l. 1056--><p class="noindent" >0.                                                                          </td>
</tr><tr  
 style="vertical-align:baseline;" id="TBL-32-13-"><td  style="white-space:nowrap; text-align:left;" id="TBL-32-13-1"  
class="td11">Status                 </td><td  style="white-space:wrap; text-align:left;" id="TBL-32-13-2"  
class="td11"><!--l. 1057--><p class="noindent" >-                                                                            </td></tr><tr  
 style="vertical-align:baseline;" id="TBL-32-14-"><td  style="white-space:nowrap; text-align:left;" id="TBL-32-14-1"  
class="td11"> </td>
</tr><tr 
class="hline"><td><hr></td><td><hr></td></tr><tr  
 style="vertical-align:baseline;" id="TBL-32-15-"><td  style="white-space:nowrap; text-align:left;" id="TBL-32-15-1"  
class="td11">                </td></tr></table></div>
<br /> <div class="caption" 
><span class="id">Table&#x00A0;31: </span><span  
class="content">Q4axisymm element summary</span></div><!--tex4ht:label?: x12-4000131 -->
                                                                                           
                                                                                           
</div><hr class="endfloat" />
</div>
</div>
<!--l. 1061--><p class="noindent" >
   <h5 class="subsubsectionHead"><span class="titlemark">2.7.3   </span> <a 
 id="x12-410002.7.3"></a>L4axisymm element</h5>
<!--l. 1062--><p class="noindent" >Implementation of isoparametric four-node quadrilateral axisymmetric finite element with linear interpolations of
displacements <span 
class="cmmi-10">u,v</span>. Node numbering and edge position is the same as in Fig.&#x00A0;<a 
href="elementlibmanualsu4.html#x9-150015">5<!--tex4ht:ref: Planestress2dfig --></a>. The element features are summarized
in Table&#x00A0;<a 
href="#x12-4100132">32<!--tex4ht:ref: l4axisymmsummary --></a>.
<div class="center" 
>
<!--l. 1065--><p class="noindent" >
<div class="table">
<!--l. 1065--><p class="noindent" ><a 
 id="x12-4100132"></a><hr class="float"><div class="float" 
> <!--tex4ht:inline--><div class="tabular"> <table id="TBL-33" class="tabular" 
cellspacing="0" cellpadding="0" rules="groups" 
><colgroup id="TBL-33-1g"><col 
id="TBL-33-1"></colgroup><colgroup id="TBL-33-2g"><col 
id="TBL-33-2"></colgroup><tr 
class="hline"><td><hr></td><td><hr></td></tr><tr  
 style="vertical-align:baseline;" id="TBL-33-1-"><td  style="white-space:nowrap; text-align:left;" id="TBL-33-1-1"  
class="td11"><span 
class="cmbx-10">Keyword         </span></td><td  style="white-space:wrap; text-align:left;" id="TBL-33-1-2"  
class="td11"><!--l. 1065--><p class="noindent" ><span 
class="cmbx-10">L4axisymm</span>                                                    </td>
</tr><tr  
 style="vertical-align:baseline;" id="TBL-33-2-"><td  style="white-space:nowrap; text-align:left;" id="TBL-33-2-1"  
class="td11">Description          </td><td  style="white-space:wrap; text-align:left;" id="TBL-33-2-2"  
class="td11"><!--l. 1065--><p class="noindent" >Isoparametric    four-node    quadrilateral    element    for
axisymmetric analysis                                                </td>
</tr><tr  
 style="vertical-align:baseline;" id="TBL-33-3-"><td  style="white-space:nowrap; text-align:left;" id="TBL-33-3-1"  
class="td11">Specific parameters</td><td  style="white-space:wrap; text-align:left;" id="TBL-33-3-2"  
class="td11"><!--l. 1065--><p class="noindent" >[<span 
class="cmtt-10">NIP</span>&#x00A0;#<span 
class="cmr-5">(in)</span>]                                                               </td>
</tr><tr 
class="hline"><td><hr></td><td><hr></td></tr><tr  
 style="vertical-align:baseline;" id="TBL-33-4-"><td  style="white-space:nowrap; text-align:left;" id="TBL-33-4-1"  
class="td11">Parameters           </td><td  style="white-space:wrap; text-align:left;" id="TBL-33-4-2"  
class="td11"><!--l. 1066--><p class="noindent" ><span 
class="cmtt-10">NIP</span>:  allows  to  set  the  number  of  integration  points  for
integration  of  terms  corresponding  to  <span 
class="cmmi-10">&#x03B5;</span><sub><span 
class="cmmi-7">x</span></sub>  and  <span 
class="cmmi-10">&#x03B5;</span><sub><span 
class="cmmi-7">y</span></sub>  strains
(possible completions are 1, 4 (default), 9, and 16).          </td>
</tr><tr  
 style="vertical-align:baseline;" id="TBL-33-5-"><td  style="white-space:nowrap; text-align:left;" id="TBL-33-5-1"  
class="td11">Unknowns            </td><td  style="white-space:wrap; text-align:left;" id="TBL-33-5-2"  
class="td11"><!--l. 1067--><p class="noindent" >Two dofs (u-displacement, v-displacement) are required in
each node.                                                               </td>
</tr><tr  
 style="vertical-align:baseline;" id="TBL-33-6-"><td  style="white-space:nowrap; text-align:left;" id="TBL-33-6-1"  
class="td11">Approximation      </td><td  style="white-space:wrap; text-align:left;" id="TBL-33-6-2"  
class="td11"><!--l. 1068--><p class="noindent" >Linear approximation of displacement and geometry.        </td>
</tr><tr  
 style="vertical-align:baseline;" id="TBL-33-7-"><td  style="white-space:nowrap; text-align:left;" id="TBL-33-7-1"  
class="td11">Integration           </td><td  style="white-space:wrap; text-align:left;" id="TBL-33-7-2"  
class="td11"><!--l. 1072--><p class="noindent" >The integration of <span 
class="cmmi-10">&#x03B5;</span><sub><span 
class="cmmi-7">x</span></sub> and <span 
class="cmmi-10">&#x03B5;</span><sub><span 
class="cmmi-7">y</span></sub> strains can be altered using <span 
class="cmtt-10">NIP</span>
parameter (possible completions are 1, 4 (default), 9 or 16
point integration rule). The remaining strain components
(<span 
class="cmmi-10">&#x03B5;</span><sub><span 
class="cmmi-7">&#x03B8;</span></sub>  and  <span 
class="cmmi-10">&gamma;</span><sub><span 
class="cmmi-7">rz</span></sub>)  are  integrated  using  one  point  integration
formula.                                                                  </td>
</tr><tr  
 style="vertical-align:baseline;" id="TBL-33-8-"><td  style="white-space:nowrap; text-align:left;" id="TBL-33-8-1"  
class="td11">Features              </td><td  style="white-space:wrap; text-align:left;" id="TBL-33-8-2"  
class="td11"><!--l. 1073--><p class="noindent" >-                                                                            </td></tr><tr  
 style="vertical-align:baseline;" id="TBL-33-9-"><td  style="white-space:nowrap; text-align:left;" id="TBL-33-9-1"  
class="td11">CS properties </td> <td  style="white-space:wrap; text-align:left;" id="TBL-33-9-2"  
class="td11"><!--l. 1074--><p class="noindent" >-</td>
</tr><tr  
 style="vertical-align:baseline;" id="TBL-33-10-"><td  style="white-space:nowrap; text-align:left;" id="TBL-33-10-1"  
class="td11">Loads                  </td><td  style="white-space:wrap; text-align:left;" id="TBL-33-10-2"  
class="td11"><!--l. 1075--><p class="noindent" >Boundary and body loads supported.                            </td>
</tr><tr  
 style="vertical-align:baseline;" id="TBL-33-11-"><td  style="white-space:nowrap; text-align:left;" id="TBL-33-11-1"  
class="td11">Nlgeo                  </td><td  style="white-space:wrap; text-align:left;" id="TBL-33-11-2"  
class="td11"><!--l. 1076--><p class="noindent" >0.                                                                          </td>
</tr><tr  
 style="vertical-align:baseline;" id="TBL-33-12-"><td  style="white-space:nowrap; text-align:left;" id="TBL-33-12-1"  
class="td11">Status                 </td><td  style="white-space:wrap; text-align:left;" id="TBL-33-12-2"  
class="td11"><!--l. 1077--><p class="noindent" >-                                                                            </td></tr><tr  
 style="vertical-align:baseline;" id="TBL-33-13-"><td  style="white-space:nowrap; text-align:left;" id="TBL-33-13-1"  
class="td11"> </td>
</tr><tr 
class="hline"><td><hr></td><td><hr></td></tr><tr  
 style="vertical-align:baseline;" id="TBL-33-14-"><td  style="white-space:nowrap; text-align:left;" id="TBL-33-14-1"  
class="td11">                </td></tr></table></div>
<br /> <div class="caption" 
><span class="id">Table&#x00A0;32: </span><span  
class="content">L4axisymm element summary</span></div><!--tex4ht:label?: x12-4100132 -->
</div><hr class="endfloat" />
</div>
</div>
                                                                                           
                                                                                           
                                                                                           
                                                                                           
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